View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 28773U 05025A 24281.15548200 .00168921 00000-0 18820-2 0 9999
2 28773 31.3833 92.0635 0005360 31.3433 328.7545 15.61197386 64423
| Epoch (UTC): | 07 October 2024 03:43:53 |
| Eccentricity: | 0.0005360 |
| inclination: | 31.3833° |
| perigee height: | 380 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 92.0635° |
| argument of perigee: | 31.3433° |
| revolutions per day: | 15.61197386 |
| mean anomaly at epoch: | 328.7545° |
| orbit number at epoch: | 6442 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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