View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52157U 26145.23374661 +.00000000 +00000-0 +21641-3 0 00000
2 52157 97.8396 224.8582 0005291 16.4034 343.7350 14.82646207 05
| Epoch (UTC): | 25 May 2026 05:36:35 |
| Eccentricity: | 0.0005291 |
| inclination: | 97.8396° |
| perigee height: | 617 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 224.8582° |
| argument of perigee: | 16.4034° |
| revolutions per day: | 14.82646207 |
| mean anomaly at epoch: | 343.7350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|