View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25991U 26106.25462105 +.00000000 +00000-0 +62016-4 0 00008
2 25991 99.0028 144.0185 0010217 172.9176 264.4593 14.17539987 00
| Epoch (UTC): | 16 April 2026 06:06:39 |
| Eccentricity: | 0.0010217 |
| inclination: | 99.0028° |
| perigee height: | 826 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 144.0185° |
| argument of perigee: | 172.9176° |
| revolutions per day: | 14.17539987 |
| mean anomaly at epoch: | 264.4593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|