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 28521U 05002A 23274.51792993 .00000109 00000-0 78901-4 0 9997
2 28521 82.9473 72.0792 0038883 271.2350 88.4359 13.87722943946877
| Epoch (UTC): | 01 October 2023 12:25:49 |
| Eccentricity: | 0.0038883 |
| inclination: | 82.9473° |
| perigee height: | 908 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 72.0792° |
| argument of perigee: | 271.2350° |
| revolutions per day: | 13.87722943 |
| mean anomaly at epoch: | 88.4359° |
| orbit number at epoch: | 94687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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