View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 05580U 26032.29282473 +.00000000 +00000-0 +31686-3 0 00008
2 05580 82.0363 50.0817 0501214 256.6993 97.7840 14.01308940 01
| Epoch (UTC): | 01 February 2026 07:01:40 |
| Eccentricity: | 0.0501214 |
| inclination: | 82.0363° |
| perigee height: | 525 km |
| apogee height: | 1254 km |
| right ascension of ascending node: | 50.0817° |
| argument of perigee: | 256.6993° |
| revolutions per day: | 14.01308940 |
| mean anomaly at epoch: | 97.7840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|