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 is defined by the following mean orbital elements,
1 30777U 07006F 22316.47588261 .34985363 19861-5 56465-3 0 9992
2 30777 35.3973 21.9825 0007116 7.3569 353.8136 16.47897565872383
| Epoch (UTC): | 12 November 2022 11:25:16 |
| Eccentricity: | 0.0007116 |
| inclination: | 35.3973° |
| perigee height: | 140 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 21.9825° |
| argument of perigee: | 7.3569° |
| revolutions per day: | 16.47897565 |
| mean anomaly at epoch: | 353.8136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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