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 14699U 84013A 25198.80107125 .00005532 00000-0 25368-3 0 9996
2 14699 82.5483 340.5867 0016244 29.6478 330.5675 15.20124616236892
| Epoch (UTC): | 17 July 2025 19:13:32 |
| Eccentricity: | 0.0016244 |
| inclination: | 82.5483° |
| perigee height: | 494 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 340.5867° |
| argument of perigee: | 29.6478° |
| revolutions per day: | 15.20124616 |
| mean anomaly at epoch: | 330.5675° |
| orbit number at epoch: | 23689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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