View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38953U 26145.38647727 +.00000000 +00000-0 +00000-0 0 00003
2 38953 4.3664 73.7642 0010337 322.0337 70.3243 1.00269605 04
| Epoch (UTC): | 25 May 2026 09:16:31 |
| Eccentricity: | 0.0010337 |
| inclination: | 4.3664° |
| perigee height: | 35744 km |
| apogee height: | 35831 km |
| right ascension of ascending node: | 73.7642° |
| argument of perigee: | 322.0337° |
| revolutions per day: | 1.00269605 |
| mean anomaly at epoch: | 70.3243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|