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 23080.57533440 .00000061 00000-0 10548-3 0 9993
2 00116 66.8079 266.0340 0073609 18.0589 342.3079 13.91896233131955
| Epoch (UTC): | 21 March 2023 13:48:28 |
| Eccentricity: | 0.0073609 |
| inclination: | 66.8079° |
| perigee height: | 868 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 266.0340° |
| argument of perigee: | 18.0589° |
| revolutions per day: | 13.91896233 |
| mean anomaly at epoch: | 342.3079° |
| orbit number at epoch: | 13195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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