View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58663U 26145.58759950 +.00000000 +00000-0 +24003-3 0 00009
2 58663 97.4470 261.7366 0005004 73.6320 286.5470 15.30684332 09
| Epoch (UTC): | 25 May 2026 14:06:08 |
| Eccentricity: | 0.0005004 |
| inclination: | 97.4470° |
| perigee height: | 470 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 261.7366° |
| argument of perigee: | 73.6320° |
| revolutions per day: | 15.30684332 |
| mean anomaly at epoch: | 286.5470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|