View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 01804U 26152.44396551 +.00000000 +00000-0 +12405-3 0 00004
2 01804 79.8010 290.0533 1329784 264.4792 80.3610 12.28329978 09
| Epoch (UTC): | 01 June 2026 10:39:18 |
| Eccentricity: | 0.1329784 |
| inclination: | 79.8010° |
| perigee height: | 501 km |
| apogee height: | 2612 km |
| right ascension of ascending node: | 290.0533° |
| argument of perigee: | 264.4792° |
| revolutions per day: | 12.28329978 |
| mean anomaly at epoch: | 80.3610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|