View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15890U 26073.62817963 +.00000000 +00000-0 +58864-4 0 00001
2 15890 82.5275 150.3172 0021339 123.4971 236.8288 14.85787126 04
| Epoch (UTC): | 14 March 2026 15:04:34 |
| Eccentricity: | 0.0021339 |
| inclination: | 82.5275° |
| perigee height: | 596 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 150.3172° |
| argument of perigee: | 123.4971° |
| revolutions per day: | 14.85787126 |
| mean anomaly at epoch: | 236.8288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|