View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 02140U 26015.53033525 +.00000000 +00000-0 +23141-3 0 00004
2 02140 89.9538 51.2215 0314257 266.2878 90.2291 13.48363154 09
| Epoch (UTC): | 15 January 2026 12:43:40 |
| Eccentricity: | 0.0314257 |
| inclination: | 89.9538° |
| perigee height: | 844 km |
| apogee height: | 1313 km |
| right ascension of ascending node: | 51.2215° |
| argument of perigee: | 266.2878° |
| revolutions per day: | 13.48363154 |
| mean anomaly at epoch: | 90.2291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|