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 24256.95146625 .00002663 00000-0 22472-2 0 9994
2 00082 38.8536 224.1214 1165329 358.3762 1.3315 12.27011599997894
| Epoch (UTC): | 12 September 2024 22:50:06 |
| Eccentricity: | 0.1165329 |
| inclination: | 38.8536° |
| perigee height: | 637 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 224.1214° |
| argument of perigee: | 358.3762° |
| revolutions per day: | 12.27011599 |
| mean anomaly at epoch: | 1.3315° |
| orbit number at epoch: | 99789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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