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 00016U 58002A 25138.30171395 .00000081 00000-0 83415-4 0 9994
2 00016 34.2822 7.0669 2023294 253.0023 84.0118 10.49574898647425
| Epoch (UTC): | 18 May 2025 07:14:28 |
| Eccentricity: | 0.2023294 |
| inclination: | 34.2822° |
| perigee height: | 650 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 7.0669° |
| argument of perigee: | 253.0023° |
| revolutions per day: | 10.49574898 |
| mean anomaly at epoch: | 84.0118° |
| orbit number at epoch: | 64742 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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