View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00012U 26133.89548552 +.00000000 +00000-0 +46401-4 0 00006
2 00012 32.9140 346.0679 1647176 283.5885 58.7124 11.48608551 06
| Epoch (UTC): | 13 May 2026 21:29:29 |
| Eccentricity: | 0.1647176 |
| inclination: | 32.9140° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 346.0679° |
| argument of perigee: | 283.5885° |
| revolutions per day: | 11.48608551 |
| mean anomaly at epoch: | 58.7124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|