View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 15598U 26088.21445528 +.00000000 +00000-0 +17454-3 0 00000
2 15598 82.9348 243.0157 0023023 137.1617 34.8535 13.76840112 03
| Epoch (UTC): | 29 March 2026 05:08:48 |
| Eccentricity: | 0.0023023 |
| inclination: | 82.9348° |
| perigee height: | 958 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 243.0157° |
| argument of perigee: | 137.1617° |
| revolutions per day: | 13.76840112 |
| mean anomaly at epoch: | 34.8535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|