View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67662U 26145.33470435 +.00000000 +00000-0 +56634-3 0 00004
2 67662 97.2844 178.6640 0001030 82.9607 277.1753 15.33447310 04
| Epoch (UTC): | 25 May 2026 08:01:58 |
| Eccentricity: | 0.0001030 |
| inclination: | 97.2844° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6640° |
| argument of perigee: | 82.9607° |
| revolutions per day: | 15.33447310 |
| mean anomaly at epoch: | 277.1753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|