View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67861U 26145.57505515 +.00000000 +00000-0 +22668-3 0 00009
2 67861 53.1587 207.3719 0000836 73.3679 286.7413 15.30209781 07
| Epoch (UTC): | 25 May 2026 13:48:04 |
| Eccentricity: | 0.0000836 |
| inclination: | 53.1587° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.3719° |
| argument of perigee: | 73.3679° |
| revolutions per day: | 15.30209781 |
| mean anomaly at epoch: | 286.7413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|