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 33498U 09002G 25173.53134937 .00002348 00000-0 23795-3 0 9997
2 33498 98.1242 103.0846 0007509 278.0620 81.9746 14.91928200885207
| Epoch (UTC): | 22 June 2025 12:45:08 |
| Eccentricity: | 0.0007509 |
| inclination: | 98.1242° |
| perigee height: | 586 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.0846° |
| argument of perigee: | 278.0620° |
| revolutions per day: | 14.91928200 |
| mean anomaly at epoch: | 81.9746° |
| orbit number at epoch: | 88520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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