View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68693U 26145.33662904 +.00000000 +00000-0 +41289-4 0 00004
2 68693 97.6610 220.8908 0015214 122.3594 237.9110 15.08642718 06
| Epoch (UTC): | 25 May 2026 08:04:44 |
| Eccentricity: | 0.0015214 |
| inclination: | 97.6610° |
| perigee height: | 530 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 220.8908° |
| argument of perigee: | 122.3594° |
| revolutions per day: | 15.08642718 |
| mean anomaly at epoch: | 237.9110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|