View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06393U 26088.11601234 +.00000000 +00000-0 +81917-4 0 00006
2 06393 81.2516 96.4132 0057474 266.7270 92.7322 14.05428751 00
| Epoch (UTC): | 29 March 2026 02:47:03 |
| Eccentricity: | 0.0057474 |
| inclination: | 81.2516° |
| perigee height: | 833 km |
| apogee height: | 917 km |
| right ascension of ascending node: | 96.4132° |
| argument of perigee: | 266.7270° |
| revolutions per day: | 14.05428751 |
| mean anomaly at epoch: | 92.7322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|