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 is defined by the following mean orbital elements,
1 38506U 99025ESR 23325.06276806 .00008775 00000-0 38358-2 0 9993
2 38506 98.9869 256.6025 0153669 260.2981 98.0808 14.17915283667044
| Epoch (UTC): | 21 November 2023 01:30:23 |
| Eccentricity: | 0.0153669 |
| inclination: | 98.9869° |
| perigee height: | 721 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 256.6025° |
| argument of perigee: | 260.2981° |
| revolutions per day: | 14.17915283 |
| mean anomaly at epoch: | 98.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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