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 00694U 63047A 25348.28014840 .00003295 00000-0 39490-3 0 9995
2 00694 30.3544 312.8537 0548930 47.7510 316.8344 14.11770329119546
| Epoch (UTC): | 14 December 2025 06:43:24 |
| Eccentricity: | 0.0548930 |
| inclination: | 30.3544° |
| perigee height: | 456 km |
| apogee height: | 1250 km |
| right ascension of ascending node: | 312.8537° |
| argument of perigee: | 47.7510° |
| revolutions per day: | 14.11770329 |
| mean anomaly at epoch: | 316.8344° |
| orbit number at epoch: | 11954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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