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 25197.13910949 .00000277 00000-0 65884-4 0 9992
2 25994 97.9964 254.1160 0002059 172.6568 240.6138 14.60733249360669
| Epoch (UTC): | 16 July 2025 03:20:19 |
| Eccentricity: | 0.0002059 |
| inclination: | 97.9964° |
| perigee height: | 689 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 254.1160° |
| argument of perigee: | 172.6568° |
| revolutions per day: | 14.60733249 |
| mean anomaly at epoch: | 240.6138° |
| orbit number at epoch: | 36066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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