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 15370U 84111B 23153.00227354 .00000569 00000-0 64720-4 0 9991
2 15370 82.5146 127.3051 0022385 78.5355 281.8373 14.84267649 86812
| Epoch (UTC): | 02 June 2023 00:03:16 |
| Eccentricity: | 0.0022385 |
| inclination: | 82.5146° |
| perigee height: | 600 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 127.3051° |
| argument of perigee: | 78.5355° |
| revolutions per day: | 14.84267649 |
| mean anomaly at epoch: | 281.8373° |
| orbit number at epoch: | 8681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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