View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67096U 26145.38037506 +.00000000 +00000-0 +31884-3 0 00008
2 67096 70.0010 181.1353 0003791 269.7223 90.3502 14.98332965 00
| Epoch (UTC): | 25 May 2026 09:07:44 |
| Eccentricity: | 0.0003791 |
| inclination: | 70.0010° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 181.1353° |
| argument of perigee: | 269.7223° |
| revolutions per day: | 14.98332965 |
| mean anomaly at epoch: | 90.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|