View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21090U 26106.61667943 +.00000000 +00000-0 +68329-4 0 00004
2 21090 82.9242 356.1538 0021160 21.7580 338.4471 13.76675165 02
| Epoch (UTC): | 16 April 2026 14:48:01 |
| Eccentricity: | 0.0021160 |
| inclination: | 82.9242° |
| perigee height: | 960 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 356.1538° |
| argument of perigee: | 21.7580° |
| revolutions per day: | 13.76675165 |
| mean anomaly at epoch: | 338.4471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|