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 33066U 08031G 25189.52305496 .00000314 00000-0 80040-4 0 9993
2 33066 48.4436 8.7468 0007274 328.4472 31.6003 14.72597658915756
| Epoch (UTC): | 08 July 2025 12:33:11 |
| Eccentricity: | 0.0007274 |
| inclination: | 48.4436° |
| perigee height: | 647 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 8.7468° |
| argument of perigee: | 328.4472° |
| revolutions per day: | 14.72597658 |
| mean anomaly at epoch: | 31.6003° |
| orbit number at epoch: | 91575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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