View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07530U 26075.89906875 +.00000000 +00000-0 +12167-3 0 00000
2 07530 101.9965 88.1666 0011933 308.1283 123.9349 12.53696576 06
| Epoch (UTC): | 16 March 2026 21:34:39 |
| Eccentricity: | 0.0011933 |
| inclination: | 101.9965° |
| perigee height: | 1440 km |
| apogee height: | 1458 km |
| right ascension of ascending node: | 88.1666° |
| argument of perigee: | 308.1283° |
| revolutions per day: | 12.53696576 |
| mean anomaly at epoch: | 123.9349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|