View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42990U 26145.34300213 +.00000000 +00000-0 +28615-3 0 00006
2 42990 97.4488 281.6933 0001653 106.5129 253.6296 15.36457551 02
| Epoch (UTC): | 25 May 2026 08:13:55 |
| Eccentricity: | 0.0001653 |
| inclination: | 97.4488° |
| perigee height: | 455 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 281.6933° |
| argument of perigee: | 106.5129° |
| revolutions per day: | 15.36457551 |
| mean anomaly at epoch: | 253.6296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|