View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67711U 26145.27566076 +.00000000 +00000-0 +57201-3 0 00000
2 67711 97.2825 256.9516 0001285 106.4760 253.6624 15.33462541 03
| Epoch (UTC): | 25 May 2026 06:36:57 |
| Eccentricity: | 0.0001285 |
| inclination: | 97.2825° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 256.9516° |
| argument of perigee: | 106.4760° |
| revolutions per day: | 15.33462541 |
| mean anomaly at epoch: | 253.6624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|