View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36597U 26044.94713235 +.00000000 +00000-0 +27682-3 0 00001
2 36597 97.9920 70.4574 0049829 333.8931 25.9780 15.02174403 05
| Epoch (UTC): | 13 February 2026 22:43:52 |
| Eccentricity: | 0.0049829 |
| inclination: | 97.9920° |
| perigee height: | 526 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 70.4574° |
| argument of perigee: | 333.8931° |
| revolutions per day: | 15.02174403 |
| mean anomaly at epoch: | 25.9780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|