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 29517U 06048B 25142.76129403 .00000098 00000-0 12248-3 0 9995
2 29517 28.2604 325.3917 4074446 52.0187 338.3226 6.89806771366879
| Epoch (UTC): | 22 May 2025 18:16:15 |
| Eccentricity: | 0.4074446 |
| inclination: | 28.2604° |
| perigee height: | 529 km |
| apogee height: | 10028 km |
| right ascension of ascending node: | 325.3917° |
| argument of perigee: | 52.0187° |
| revolutions per day: | 6.89806771 |
| mean anomaly at epoch: | 338.3226° |
| orbit number at epoch: | 36687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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