View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 69012U 26145.24890612 +.00000000 +00000-0 +16334-3 0 00001
2 69012 97.4065 43.4893 0007146 108.2594 251.9420 15.20491322 01
| Epoch (UTC): | 25 May 2026 05:58:25 |
| Eccentricity: | 0.0007146 |
| inclination: | 97.4065° |
| perigee height: | 499 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 43.4893° |
| argument of perigee: | 108.2594° |
| revolutions per day: | 15.20491322 |
| mean anomaly at epoch: | 251.9420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|