View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53476U 26145.28626794 +.00000000 +00000-0 +88444-4 0 00002
2 53476 97.4525 265.3098 0001285 134.1641 225.9692 15.05663598 01
| Epoch (UTC): | 25 May 2026 06:52:13 |
| Eccentricity: | 0.0001285 |
| inclination: | 97.4525° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.3098° |
| argument of perigee: | 134.1641° |
| revolutions per day: | 15.05663598 |
| mean anomaly at epoch: | 225.9692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|