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 24284.54265944 .00120067 00000-0 12938-2 0 9999
2 28773 31.3831 68.5100 0005118 59.3596 300.7568 15.62203023 64935
| Epoch (UTC): | 10 October 2024 13:01:25 |
| Eccentricity: | 0.0005118 |
| inclination: | 31.3831° |
| perigee height: | 378 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 68.5100° |
| argument of perigee: | 59.3596° |
| revolutions per day: | 15.62203023 |
| mean anomaly at epoch: | 300.7568° |
| orbit number at epoch: | 6493 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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