View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 62282U 26145.46430600 +.00000000 +00000-0 +51920-3 0 00004
2 62282 43.0010 142.7710 0001977 269.6348 90.4277 15.27592317 05
| Epoch (UTC): | 25 May 2026 11:08:36 |
| Eccentricity: | 0.0001977 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.7710° |
| argument of perigee: | 269.6348° |
| revolutions per day: | 15.27592317 |
| mean anomaly at epoch: | 90.4277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|