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 25173.36704650 -.00000007 00000-0 53443-4 0 9991
2 00116 66.8103 51.2182 0073831 170.7211 189.5253 13.92243781246616
| Epoch (UTC): | 22 June 2025 08:48:32 |
| Eccentricity: | 0.0073831 |
| inclination: | 66.8103° |
| perigee height: | 867 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 51.2182° |
| argument of perigee: | 170.7211° |
| revolutions per day: | 13.92243781 |
| mean anomaly at epoch: | 189.5253° |
| orbit number at epoch: | 24661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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