View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00115U 26132.75852994 +.00000000 +00000-0 +20200-3 0 00000
2 00115 48.1628 275.1410 0025445 99.3104 261.0693 14.98005330 04
| Epoch (UTC): | 12 May 2026 18:12:16 |
| Eccentricity: | 0.0025445 |
| inclination: | 48.1628° |
| perigee height: | 555 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 275.1410° |
| argument of perigee: | 99.3104° |
| revolutions per day: | 14.98005330 |
| mean anomaly at epoch: | 261.0693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|