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 25544U 98067A 25140.21045238 .00008546 00000-0 15962-3 0 9996
2 25544 51.6372 85.6698 0002547 123.7739 203.9910 15.49623238510810
| Epoch (UTC): | 20 May 2025 05:03:03 |
| Eccentricity: | 0.0002547 |
| inclination: | 51.6372° |
| perigee height: | 416 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 85.6698° |
| argument of perigee: | 123.7739° |
| revolutions per day: | 15.49623238 |
| mean anomaly at epoch: | 203.9910° |
| orbit number at epoch: | 51081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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