View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59637U 26145.11989302 +.00000000 +00000-0 -54527-4 0 00002
2 59637 43.0042 67.9394 0001227 287.7489 72.3229 15.27596321 06
| Epoch (UTC): | 25 May 2026 02:52:38 |
| Eccentricity: | 0.0001227 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 67.9394° |
| argument of perigee: | 287.7489° |
| revolutions per day: | 15.27596321 |
| mean anomaly at epoch: | 72.3229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|