View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29092U 26068.48510374 +.00000000 +00000-0 +13870-3 0 00001
2 29092 97.7556 91.7240 0001477 93.9386 266.2000 14.87584438 01
| Epoch (UTC): | 09 March 2026 11:38:32 |
| Eccentricity: | 0.0001477 |
| inclination: | 97.7556° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 91.7240° |
| argument of perigee: | 93.9386° |
| revolutions per day: | 14.87584438 |
| mean anomaly at epoch: | 266.2000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|