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 00876U 64053A 23156.55730470 .00000106 00000-0 40284-4 0 9996
2 00876 65.0609 354.9811 0145665 330.6645 28.6333 14.64218045126418
| Epoch (UTC): | 05 June 2023 13:22:31 |
| Eccentricity: | 0.0145665 |
| inclination: | 65.0609° |
| perigee height: | 577 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 354.9811° |
| argument of perigee: | 330.6645° |
| revolutions per day: | 14.64218045 |
| mean anomaly at epoch: | 28.6333° |
| orbit number at epoch: | 12641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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