View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37756U 26070.18349382 +.00000000 +00000-0 +85829-3 0 00009
2 37756 51.4394 1.9504 1812497 178.8096 181.7996 11.46810184 01
| Epoch (UTC): | 11 March 2026 04:24:13 |
| Eccentricity: | 0.1812497 |
| inclination: | 51.4394° |
| perigee height: | 423 km |
| apogee height: | 3434 km |
| right ascension of ascending node: | 1.9504° |
| argument of perigee: | 178.8096° |
| revolutions per day: | 11.46810184 |
| mean anomaly at epoch: | 181.7996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|