View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27598U 26100.14677987 +.00000000 +00000-0 +68318-4 0 00002
2 27598 98.8546 72.4241 0009058 169.2379 190.8997 14.29712421 08
| Epoch (UTC): | 10 April 2026 03:31:21 |
| Eccentricity: | 0.0009058 |
| inclination: | 98.8546° |
| perigee height: | 786 km |
| apogee height: | 799 km |
| right ascension of ascending node: | 72.4241° |
| argument of perigee: | 169.2379° |
| revolutions per day: | 14.29712421 |
| mean anomaly at epoch: | 190.8997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|