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 32788U 08021F 23089.46177914 .00017247 00000-0 13158-2 0 9991
2 32788 97.5579 70.7628 0004373 250.0617 110.0137 15.02062038811381
| Epoch (UTC): | 30 March 2023 11:04:57 |
| Eccentricity: | 0.0004373 |
| inclination: | 97.5579° |
| perigee height: | 557 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 70.7628° |
| argument of perigee: | 250.0617° |
| revolutions per day: | 15.02062038 |
| mean anomaly at epoch: | 110.0137° |
| orbit number at epoch: | 81138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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