View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64692U 26087.89023506 +.00000000 +00000-0 +39408-3 0 00003
2 64692 95.9939 229.4913 0015886 104.2053 256.0926 14.73323949 01
| Epoch (UTC): | 28 March 2026 21:21:56 |
| Eccentricity: | 0.0015886 |
| inclination: | 95.9939° |
| perigee height: | 639 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 229.4913° |
| argument of perigee: | 104.2053° |
| revolutions per day: | 14.73323949 |
| mean anomaly at epoch: | 256.0926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|