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 25133.81236691 .00000499 00000-0 45417-3 0 9997
2 00082 38.8564 42.9539 1166577 93.0258 280.4239 12.27627083 27711
| Epoch (UTC): | 13 May 2025 19:29:48 |
| Eccentricity: | 0.1166577 |
| inclination: | 38.8564° |
| perigee height: | 633 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 42.9539° |
| argument of perigee: | 93.0258° |
| revolutions per day: | 12.27627083 |
| mean anomaly at epoch: | 280.4239° |
| orbit number at epoch: | 2771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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