View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68230U 26145.62475454 +.00000000 +00000-0 +33691-3 0 00002
2 68230 97.2868 21.1457 0001679 94.5958 265.5477 15.33436299 05
| Epoch (UTC): | 25 May 2026 14:59:38 |
| Eccentricity: | 0.0001679 |
| inclination: | 97.2868° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 21.1457° |
| argument of perigee: | 94.5958° |
| revolutions per day: | 15.33436299 |
| mean anomaly at epoch: | 265.5477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|