View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 14440U 26087.72653311 +.00000000 +00000-0 +91020-3 0 00002
2 14440 82.9165 255.1426 0112299 270.1379 110.7773 13.64390889 01
| Epoch (UTC): | 28 March 2026 17:26:12 |
| Eccentricity: | 0.0112299 |
| inclination: | 82.9165° |
| perigee height: | 937 km |
| apogee height: | 1103 km |
| right ascension of ascending node: | 255.1426° |
| argument of perigee: | 270.1379° |
| revolutions per day: | 13.64390889 |
| mean anomaly at epoch: | 110.7773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|