View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67929U 26145.45163764 +.00000000 +00000-0 +90125-4 0 00001
2 67929 43.0027 171.5881 0001470 263.9083 96.1601 15.27570488 05
| Epoch (UTC): | 25 May 2026 10:50:21 |
| Eccentricity: | 0.0001470 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.5881° |
| argument of perigee: | 263.9083° |
| revolutions per day: | 15.27570488 |
| mean anomaly at epoch: | 96.1601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|