View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58979U 26144.92747015 +.00000000 +00000-0 +46508-4 0 00000
2 58979 53.1616 302.7072 0000998 75.6127 284.4985 15.30197968 06
| Epoch (UTC): | 24 May 2026 22:15:33 |
| Eccentricity: | 0.0000998 |
| inclination: | 53.1616° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 302.7072° |
| argument of perigee: | 75.6127° |
| revolutions per day: | 15.30197968 |
| mean anomaly at epoch: | 284.4985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|