View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15362U 26053.85559860 +.00000000 +00000-0 +10814-3 0 00009
2 15362 90.1136 81.3546 0033082 128.6179 50.4678 13.23054714 06
| Epoch (UTC): | 22 February 2026 20:32:03 |
| Eccentricity: | 0.0033082 |
| inclination: | 90.1136° |
| perigee height: | 1148 km |
| apogee height: | 1198 km |
| right ascension of ascending node: | 81.3546° |
| argument of perigee: | 128.6179° |
| revolutions per day: | 13.23054714 |
| mean anomaly at epoch: | 50.4678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|