View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11964U 26053.02765200 +.00000000 +00000-0 +00000-0 0 00002
2 11964 8.2342 303.8065 0031857 102.5650 101.9533 0.99233653 02
| Epoch (UTC): | 22 February 2026 00:39:49 |
| Eccentricity: | 0.0031857 |
| inclination: | 8.2342° |
| perigee height: | 35945 km |
| apogee height: | 36215 km |
| right ascension of ascending node: | 303.8065° |
| argument of perigee: | 102.5650° |
| revolutions per day: | 0.99233653 |
| mean anomaly at epoch: | 101.9533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|