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 24278U 96046B 23155.91661033 -.00000018 00000-0 14418-4 0 9995
2 24278 98.5277 136.1448 0351327 88.7246 275.4110 13.53145399323276
| Epoch (UTC): | 04 June 2023 21:59:55 |
| Eccentricity: | 0.0351327 |
| inclination: | 98.5277° |
| perigee height: | 799 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 136.1448° |
| argument of perigee: | 88.7246° |
| revolutions per day: | 13.53145399 |
| mean anomaly at epoch: | 275.4110° |
| orbit number at epoch: | 32327 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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