View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07575U 26040.25355407 +.00000000 +00000-0 +52904-5 0 00005
2 07575 81.2456 113.4027 0049082 313.3222 46.3862 14.11555644 04
| Epoch (UTC): | 09 February 2026 06:05:07 |
| Eccentricity: | 0.0049082 |
| inclination: | 81.2456° |
| perigee height: | 819 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 113.4027° |
| argument of perigee: | 313.3222° |
| revolutions per day: | 14.11555644 |
| mean anomaly at epoch: | 46.3862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|