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 00877U 64053B 23150.11642469 .00000246 00000-0 74230-4 0 9996
2 00877 65.0788 62.0368 0074263 324.9474 34.6749 14.59849050118613
| Epoch (UTC): | 30 May 2023 02:47:39 |
| Eccentricity: | 0.0074263 |
| inclination: | 65.0788° |
| perigee height: | 641 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 62.0368° |
| argument of perigee: | 324.9474° |
| revolutions per day: | 14.59849050 |
| mean anomaly at epoch: | 34.6749° |
| orbit number at epoch: | 11861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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