View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 36597U 26064.66320573 +.00000000 +00000-0 +26865-3 0 00003
2 36597 97.9910 90.7740 0047681 266.8212 92.7556 15.02305268 03
| Epoch (UTC): | 05 March 2026 15:55:00 |
| Eccentricity: | 0.0047681 |
| inclination: | 97.9910° |
| perigee height: | 527 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 90.7740° |
| argument of perigee: | 266.8212° |
| revolutions per day: | 15.02305268 |
| mean anomaly at epoch: | 92.7556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|