View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 12987U 26067.24393080 +.00000000 +00000-0 +57770-3 0 00009
2 12987 82.4944 351.9779 0010691 173.2444 186.8945 15.33858701 05
| Epoch (UTC): | 08 March 2026 05:51:15 |
| Eccentricity: | 0.0010691 |
| inclination: | 82.4944° |
| perigee height: | 457 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 351.9779° |
| argument of perigee: | 173.2444° |
| revolutions per day: | 15.33858701 |
| mean anomaly at epoch: | 186.8945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|