View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10489U 26106.72896648 +.00000000 +00000-0 +00000-0 0 00000
2 10489 5.2304 281.8682 0010915 92.5640 109.5223 1.00306767 07
| Epoch (UTC): | 16 April 2026 17:29:42 |
| Eccentricity: | 0.0010915 |
| inclination: | 5.2304° |
| perigee height: | 35731 km |
| apogee height: | 35823 km |
| right ascension of ascending node: | 281.8682° |
| argument of perigee: | 92.5640° |
| revolutions per day: | 1.00306767 |
| mean anomaly at epoch: | 109.5223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|