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 28932U 06002B 25194.57747572 .00003961 00000-0 23095-3 0 9998
2 28932 98.2157 317.5517 0057476 333.3342 26.4933 15.11256148 58360
| Epoch (UTC): | 13 July 2025 13:51:33 |
| Eccentricity: | 0.0057476 |
| inclination: | 98.2157° |
| perigee height: | 492 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 317.5517° |
| argument of perigee: | 333.3342° |
| revolutions per day: | 15.11256148 |
| mean anomaly at epoch: | 26.4933° |
| orbit number at epoch: | 5836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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