View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67702U 26145.54755867 +.00000000 +00000-0 +56044-3 0 00002
2 67702 97.2840 257.1906 0000444 114.8093 245.3196 15.33448806 04
| Epoch (UTC): | 25 May 2026 13:08:29 |
| Eccentricity: | 0.0000444 |
| inclination: | 97.2840° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1906° |
| argument of perigee: | 114.8093° |
| revolutions per day: | 15.33448806 |
| mean anomaly at epoch: | 245.3196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|