View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08845U 26088.19013707 +.00000000 +00000-0 -23179-4 0 00007
2 08845 81.2646 33.7013 0039893 157.9413 202.3487 14.11826430 09
| Epoch (UTC): | 29 March 2026 04:33:47 |
| Eccentricity: | 0.0039893 |
| inclination: | 81.2646° |
| perigee height: | 824 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 33.7013° |
| argument of perigee: | 157.9413° |
| revolutions per day: | 14.11826430 |
| mean anomaly at epoch: | 202.3487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|