View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67863U 26145.43809461 +.00000000 +00000-0 +43482-3 0 00000
2 67863 53.1598 207.9379 0000850 63.6189 296.4899 15.30203836 04
| Epoch (UTC): | 25 May 2026 10:30:51 |
| Eccentricity: | 0.0000850 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9379° |
| argument of perigee: | 63.6189° |
| revolutions per day: | 15.30203836 |
| mean anomaly at epoch: | 296.4899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|