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 116U 61015A 23088.26374170 .00000141 00000-0 16670-3 0 9991
2 116 66.8084 247.2334 0074210 12.5212 347.7689 13.91899346133525
| Epoch (UTC): | 29 March 2023 06:19:47 |
| Eccentricity: | 0.0074210 |
| inclination: | 66.8084° |
| perigee height: | 868 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 247.2334° |
| argument of perigee: | 12.5212° |
| revolutions per day: | 13.91899346 |
| mean anomaly at epoch: | 347.7689° |
| orbit number at epoch: | 13352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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