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 28647U 05016B 25189.17823703 .00007226 00000-0 21756-3 0 9996
2 28647 56.9997 209.8389 0069057 273.9416 85.3742 15.33172988339441
| Epoch (UTC): | 08 July 2025 04:16:39 |
| Eccentricity: | 0.0069057 |
| inclination: | 56.9997° |
| perigee height: | 419 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 209.8389° |
| argument of perigee: | 273.9416° |
| revolutions per day: | 15.33172988 |
| mean anomaly at epoch: | 85.3742° |
| orbit number at epoch: | 33944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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