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 00116U 61015A 25188.88376581 .00000004 00000-0 62001-4 0 9998
2 00116 66.8104 13.2547 0072664 159.5694 200.8319 13.92245818248775
| Epoch (UTC): | 07 July 2025 21:12:37 |
| Eccentricity: | 0.0072664 |
| inclination: | 66.8104° |
| perigee height: | 868 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 13.2547° |
| argument of perigee: | 159.5694° |
| revolutions per day: | 13.92245818 |
| mean anomaly at epoch: | 200.8319° |
| orbit number at epoch: | 24877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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