View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21015U 26100.12140199 +.00000000 +00000-0 +72554-4 0 00005
2 21015 74.0520 350.2384 0021682 180.6996 179.4132 14.37289928 02
| Epoch (UTC): | 10 April 2026 02:54:49 |
| Eccentricity: | 0.0021682 |
| inclination: | 74.0520° |
| perigee height: | 752 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 350.2384° |
| argument of perigee: | 180.6996° |
| revolutions per day: | 14.37289928 |
| mean anomaly at epoch: | 179.4132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|