View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67977U 26145.43986464 +.00000000 +00000-0 +49998-3 0 00003
2 67977 97.2839 155.4983 0000859 72.9306 287.2031 15.33458350 00
| Epoch (UTC): | 25 May 2026 10:33:24 |
| Eccentricity: | 0.0000859 |
| inclination: | 97.2839° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.4983° |
| argument of perigee: | 72.9306° |
| revolutions per day: | 15.33458350 |
| mean anomaly at epoch: | 287.2031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|