View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 13819U 26021.49736155 +.00000000 +00000-0 +37460-3 0 00009
2 13819 81.1017 60.0412 0016556 206.8652 153.1736 15.44695172 07
| Epoch (UTC): | 21 January 2026 11:56:12 |
| Eccentricity: | 0.0016556 |
| inclination: | 81.1017° |
| perigee height: | 421 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 60.0412° |
| argument of perigee: | 206.8652° |
| revolutions per day: | 15.44695172 |
| mean anomaly at epoch: | 153.1736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|