View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00012U 26137.80903605 +.00000000 +00000-0 +54575-4 0 00006
2 00012 32.9115 332.2783 1647105 304.3055 41.2187 11.48609206 08
| Epoch (UTC): | 17 May 2026 19:25:00 |
| Eccentricity: | 0.1647105 |
| inclination: | 32.9115° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 332.2783° |
| argument of perigee: | 304.3055° |
| revolutions per day: | 11.48609206 |
| mean anomaly at epoch: | 41.2187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|