View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68995U 26145.26877711 +.00000000 +00000-0 +27722-3 0 00000
2 68995 97.7392 43.1491 0002143 159.9932 200.1371 14.91641916 02
| Epoch (UTC): | 25 May 2026 06:27:02 |
| Eccentricity: | 0.0002143 |
| inclination: | 97.7392° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.1491° |
| argument of perigee: | 159.9932° |
| revolutions per day: | 14.91641916 |
| mean anomaly at epoch: | 200.1371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|