View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 04071U 26159.47449073 +.00000000 +00000-0 +13733-3 0 00006
2 04071 74.0486 313.4946 0013405 170.7350 189.4069 14.66697574 01
| Epoch (UTC): | 08 June 2026 11:23:15 |
| Eccentricity: | 0.0013405 |
| inclination: | 74.0486° |
| perigee height: | 662 km |
| apogee height: | 681 km |
| right ascension of ascending node: | 313.4946° |
| argument of perigee: | 170.7350° |
| revolutions per day: | 14.66697574 |
| mean anomaly at epoch: | 189.4069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|