View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68287U 26145.20323230 +.00000000 +00000-0 +60983-3 0 00006
2 68287 53.1584 322.5574 0001128 88.3094 271.8038 15.34411968 02
| Epoch (UTC): | 25 May 2026 04:52:39 |
| Eccentricity: | 0.0001128 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 322.5574° |
| argument of perigee: | 88.3094° |
| revolutions per day: | 15.34411968 |
| mean anomaly at epoch: | 271.8038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|