View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67871U 26145.47386134 +.00000000 +00000-0 +49856-3 0 00001
2 67871 53.1565 207.4439 0001630 94.0076 266.1111 15.30203721 03
| Epoch (UTC): | 25 May 2026 11:22:21 |
| Eccentricity: | 0.0001630 |
| inclination: | 53.1565° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.4439° |
| argument of perigee: | 94.0076° |
| revolutions per day: | 15.30203721 |
| mean anomaly at epoch: | 266.1111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|