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 00082U 61004B 25167.57397241 .00000242 00000-0 21871-3 0 9990
2 00082 38.8641 277.6100 1168238 256.3956 90.4202 12.27656148 31867
| Epoch (UTC): | 16 June 2025 13:46:31 |
| Eccentricity: | 0.1168238 |
| inclination: | 38.8641° |
| perigee height: | 632 km |
| apogee height: | 2486 km |
| right ascension of ascending node: | 277.6100° |
| argument of perigee: | 256.3956° |
| revolutions per day: | 12.27656148 |
| mean anomaly at epoch: | 90.4202° |
| orbit number at epoch: | 3186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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