View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19046U 26020.92600279 +.00000000 +00000-0 +51274-3 0 00000
2 19046 97.5123 4.3963 0027830 43.6718 316.6711 15.19220311 03
| Epoch (UTC): | 20 January 2026 22:13:26 |
| Eccentricity: | 0.0027830 |
| inclination: | 97.5123° |
| perigee height: | 489 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 4.3963° |
| argument of perigee: | 43.6718° |
| revolutions per day: | 15.19220311 |
| mean anomaly at epoch: | 316.6711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|