View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10953U 26141.99926119 +.00000000 +00000-0 +00000-0 0 00001
2 10953 6.9614 299.5494 0001202 4.5695 196.0508 0.99357814 07
| Epoch (UTC): | 21 May 2026 23:58:56 |
| Eccentricity: | 0.0001202 |
| inclination: | 6.9614° |
| perigee height: | 36040 km |
| apogee height: | 36050 km |
| right ascension of ascending node: | 299.5494° |
| argument of perigee: | 4.5695° |
| revolutions per day: | 0.99357814 |
| mean anomaly at epoch: | 196.0508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|