View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25397U 26087.98692605 +.00000000 +00000-0 +62958-4 0 00001
2 25397 99.0048 78.7352 0002345 88.2224 271.9223 14.24411200 05
| Epoch (UTC): | 28 March 2026 23:41:10 |
| Eccentricity: | 0.0002345 |
| inclination: | 99.0048° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 78.7352° |
| argument of perigee: | 88.2224° |
| revolutions per day: | 14.24411200 |
| mean anomaly at epoch: | 271.9223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|