View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62103U 26145.44640205 +.00000000 +00000-0 +46468-3 0 00009
2 62103 42.9996 131.7600 0001341 270.1063 89.9635 15.27592701 08
| Epoch (UTC): | 25 May 2026 10:42:49 |
| Eccentricity: | 0.0001341 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.7600° |
| argument of perigee: | 270.1063° |
| revolutions per day: | 15.27592701 |
| mean anomaly at epoch: | 89.9635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|