View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19468U 26088.17681338 +.00000000 +00000-0 -15294-3 0 00007
2 19468 98.9678 137.9628 0071720 153.1253 257.0659 14.03762155 08
| Epoch (UTC): | 29 March 2026 04:14:36 |
| Eccentricity: | 0.0071720 |
| inclination: | 98.9678° |
| perigee height: | 829 km |
| apogee height: | 933 km |
| right ascension of ascending node: | 137.9628° |
| argument of perigee: | 153.1253° |
| revolutions per day: | 14.03762155 |
| mean anomaly at epoch: | 257.0659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|