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 25994U 99068A 25119.19070313 .00000902 00000-0 19456-3 0 9992
2 25994 98.0016 178.8109 0003704 95.5607 349.2580 14.60653230349282
| Epoch (UTC): | 29 April 2025 04:34:36 |
| Eccentricity: | 0.0003704 |
| inclination: | 98.0016° |
| perigee height: | 688 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 178.8109° |
| argument of perigee: | 95.5607° |
| revolutions per day: | 14.60653230 |
| mean anomaly at epoch: | 349.2580° |
| orbit number at epoch: | 34928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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