View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29108U 26160.53393604 +.00000000 +00000-0 +16223-3 0 00008
2 29108 98.4470 175.9368 0001055 76.7434 283.3888 14.69334281 06
| Epoch (UTC): | 09 June 2026 12:48:52 |
| Eccentricity: | 0.0001055 |
| inclination: | 98.4470° |
| perigee height: | 662 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 175.9368° |
| argument of perigee: | 76.7434° |
| revolutions per day: | 14.69334281 |
| mean anomaly at epoch: | 283.3888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|