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 25173.61965238 -.00000065 00000-0 -63216-4 0 9995
2 00016 34.2621 264.9365 2023057 42.1295 331.8275 10.49574382651132
| Epoch (UTC): | 22 June 2025 14:52:17 |
| Eccentricity: | 0.2023057 |
| inclination: | 34.2621° |
| perigee height: | 651 km |
| apogee height: | 4216 km |
| right ascension of ascending node: | 264.9365° |
| argument of perigee: | 42.1295° |
| revolutions per day: | 10.49574382 |
| mean anomaly at epoch: | 331.8275° |
| orbit number at epoch: | 65113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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