View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37210U 26145.54415935 +.00000000 +00000-0 +00000-0 0 00000
2 37210 3.5933 69.0824 0005465 207.9169 322.0150 1.00271900 04
| Epoch (UTC): | 25 May 2026 13:03:35 |
| Eccentricity: | 0.0005465 |
| inclination: | 3.5933° |
| perigee height: | 35764 km |
| apogee height: | 35810 km |
| right ascension of ascending node: | 69.0824° |
| argument of perigee: | 207.9169° |
| revolutions per day: | 1.00271900 |
| mean anomaly at epoch: | 322.0150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|