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 28537U 05004A 23251.79660217 0.00000040 00000-0 37802-4 0 06
2 28537 63.4120 140.3487 0468916 0.5977 359.4023 13.40897329 04
| Epoch (UTC): | 08 September 2023 19:07:06 |
| Eccentricity: | 0.0468916 |
| inclination: | 63.4120° |
| perigee height: | 755 km |
| apogee height: | 1457 km |
| right ascension of ascending node: | 140.3487° |
| argument of perigee: | 0.5977° |
| revolutions per day: | 13.40897329 |
| mean anomaly at epoch: | 359.4023° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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