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 23151.41862887 .00006236 00000-0 25876-3 0 9993
2 15369 82.5232 138.1642 0012272 258.5980 101.3878 15.23598932110146
| Epoch (UTC): | 31 May 2023 10:02:49 |
| Eccentricity: | 0.0012272 |
| inclination: | 82.5232° |
| perigee height: | 486 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 138.1642° |
| argument of perigee: | 258.5980° |
| revolutions per day: | 15.23598932 |
| mean anomaly at epoch: | 101.3878° |
| orbit number at epoch: | 11014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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