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 25188.50947518 .00000045 00000-0 47300-4 0 9999
2 28654 98.8422 267.6717 0015065 53.5203 306.7356 14.13617172 37699
| Epoch (UTC): | 07 July 2025 12:13:38 |
| Eccentricity: | 0.0015065 |
| inclination: | 98.8422° |
| perigee height: | 836 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 267.6717° |
| argument of perigee: | 53.5203° |
| revolutions per day: | 14.13617172 |
| mean anomaly at epoch: | 306.7356° |
| orbit number at epoch: | 3769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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