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 28654U 05018A 25173.15020565 .00000067 00000-0 58752-4 0 9995
2 28654 98.8423 252.4853 0015378 94.1939 266.0992 14.13613987 35521
| Epoch (UTC): | 22 June 2025 03:36:17 |
| Eccentricity: | 0.0015378 |
| inclination: | 98.8423° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 252.4853° |
| argument of perigee: | 94.1939° |
| revolutions per day: | 14.13613987 |
| mean anomaly at epoch: | 266.0992° |
| orbit number at epoch: | 3552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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