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 23533U 95015A 23088.56634946 .00000486 00000-0 26805-3 0 9992
2 23533 98.8277 96.9876 0005707 272.5267 197.2246 14.16165756446742
| Epoch (UTC): | 29 March 2023 13:35:32 |
| Eccentricity: | 0.0005707 |
| inclination: | 98.8277° |
| perigee height: | 834 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 96.9876° |
| argument of perigee: | 272.5267° |
| revolutions per day: | 14.16165756 |
| mean anomaly at epoch: | 197.2246° |
| orbit number at epoch: | 44674 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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