View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 24971U 26072.91758784 +.00000000 +00000-0 +10314-3 0 00004
2 24971 98.8398 64.9568 0052680 147.4326 213.0127 14.35472679 00
| Epoch (UTC): | 13 March 2026 22:01:19 |
| Eccentricity: | 0.0052680 |
| inclination: | 98.8398° |
| perigee height: | 736 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 64.9568° |
| argument of perigee: | 147.4326° |
| revolutions per day: | 14.35472679 |
| mean anomaly at epoch: | 213.0127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|