View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62842U 26145.65801503 +.00000000 +00000-0 +98606-3 0 00003
2 62842 43.0021 7.2610 0001847 254.9324 105.1323 15.27629351 05
| Epoch (UTC): | 25 May 2026 15:47:32 |
| Eccentricity: | 0.0001847 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 7.2610° |
| argument of perigee: | 254.9324° |
| revolutions per day: | 15.27629351 |
| mean anomaly at epoch: | 105.1323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|