View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67583U 26145.44539103 +.00000000 +00000-0 +53402-3 0 00006
2 67583 97.2848 205.8712 0000622 101.2812 258.8501 15.33456101 07
| Epoch (UTC): | 25 May 2026 10:41:21 |
| Eccentricity: | 0.0000622 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.8712° |
| argument of perigee: | 101.2812° |
| revolutions per day: | 15.33456101 |
| mean anomaly at epoch: | 258.8501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|