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 15369U 84111A 23156.47558398 .00006527 00000-0 27039-3 0 9999
2 15369 82.5239 133.1258 0012481 238.1026 121.8997 15.23662662110914
| Epoch (UTC): | 05 June 2023 11:24:50 |
| Eccentricity: | 0.0012481 |
| inclination: | 82.5239° |
| perigee height: | 486 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 133.1258° |
| argument of perigee: | 238.1026° |
| revolutions per day: | 15.23662662 |
| mean anomaly at epoch: | 121.8997° |
| orbit number at epoch: | 11091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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