View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68101U 26145.39503615 +.00000000 +00000-0 +73999-3 0 00009
2 68101 97.2848 105.9483 0001873 96.1411 264.0045 15.33448637 02
| Epoch (UTC): | 25 May 2026 09:28:51 |
| Eccentricity: | 0.0001873 |
| inclination: | 97.2848° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 105.9483° |
| argument of perigee: | 96.1411° |
| revolutions per day: | 15.33448637 |
| mean anomaly at epoch: | 264.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|