View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42991U 26145.66145469 +.00000000 +00000-0 +29233-3 0 00009
2 42991 97.4500 283.0039 0006271 175.0358 185.0950 15.36404830 04
| Epoch (UTC): | 25 May 2026 15:52:29 |
| Eccentricity: | 0.0006271 |
| inclination: | 97.4500° |
| perigee height: | 452 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 283.0039° |
| argument of perigee: | 175.0358° |
| revolutions per day: | 15.36404830 |
| mean anomaly at epoch: | 185.0950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|