View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68285U 26145.50211440 +.00000000 +00000-0 +99213-3 0 00004
2 68285 53.1591 323.0192 0001081 100.7971 259.3151 15.30215937 02
| Epoch (UTC): | 25 May 2026 12:03:02 |
| Eccentricity: | 0.0001081 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.0192° |
| argument of perigee: | 100.7971° |
| revolutions per day: | 15.30215937 |
| mean anomaly at epoch: | 259.3151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|