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 35519U 87068CN 23156.77223500 .00006979 00000-0 20713-2 0 9991
2 35519 82.8358 270.9171 0017648 261.9251 97.9940 14.43093619980069
| Epoch (UTC): | 05 June 2023 18:32:01 |
| Eccentricity: | 0.0017648 |
| inclination: | 82.8358° |
| perigee height: | 736 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 270.9171° |
| argument of perigee: | 261.9251° |
| revolutions per day: | 14.43093619 |
| mean anomaly at epoch: | 97.9940° |
| orbit number at epoch: | 98006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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