View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68687U 26121.56499271 +.00000000 +00000-0 +35284-3 0 00008
2 68687 86.4967 298.5999 0001401 91.1620 268.9698 13.65394683 09
| Epoch (UTC): | 01 May 2026 13:33:35 |
| Eccentricity: | 0.0001401 |
| inclination: | 86.4967° |
| perigee height: | 1015 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 298.5999° |
| argument of perigee: | 91.1620° |
| revolutions per day: | 13.65394683 |
| mean anomaly at epoch: | 268.9698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|