
LRE [NASDA]
Initially, LRE (Laser Ranging Equipment) was used to evaluate the accuracy of the initial trajectory determination of the H-2A-202 launch vehicle. Subsequently, the satellite was used to verify SLR station performance, as a target for wide dynamic range of transmitting/receiving tests up to geosynchronous orbit for optical communication and SLR, and to evaluate the air drag model using SLR data.
Retroreflector Array Characteristics:
The array consists of 126 cube corners and 24 plate mirrors. There are two kinds of cube
corners (fused silica and BK7). Approximate center of mass correction is 210 mm.
| Nation: | Japan |
|---|---|
| Type / Application: | Geodesy |
| Operator: | NASDA |
| Contractors: | NASDA |
| Equipment: | Retrorelector Array and plate mirrors |
| Configuration: | 47 cm Sphere |
| Propulsion: | None |
| Power: | None |
| Lifetime: | |
| Mass: | 86 kg |
| Orbit: | 272 km × 36215 km, 28.15 |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| LRE | 2001-038A | 29.08.2001 | Ta YLP-1 | H-2A-202 | with VEP 2 |
