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 01778U 65096A 25118.21316844 .00000531 00000-0 14332-3 0 9990
2 01778 34.2545 82.0788 0741352 147.7944 217.0266 13.49280454908707
| Epoch (UTC): | 28 April 2025 05:06:57 |
| Eccentricity: | 0.0741352 |
| inclination: | 34.2545° |
| perigee height: | 522 km |
| apogee height: | 1627 km |
| right ascension of ascending node: | 82.0788° |
| argument of perigee: | 147.7944° |
| revolutions per day: | 13.49280454 |
| mean anomaly at epoch: | 217.0266° |
| orbit number at epoch: | 90870 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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