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 33499U 09002H 25118.78524374 .00003127 00000-0 40591-3 0 9991
2 33499 98.1224 30.2844 0007897 181.6874 178.4313 14.81472541874804
| Epoch (UTC): | 28 April 2025 18:50:45 |
| Eccentricity: | 0.0007897 |
| inclination: | 98.1224° |
| perigee height: | 619 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 30.2844° |
| argument of perigee: | 181.6874° |
| revolutions per day: | 14.81472541 |
| mean anomaly at epoch: | 178.4313° |
| orbit number at epoch: | 87480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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