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 37386U 11014A 23268.99285902 0.00000000 00000-0 00000-0 0 02
2 37386 63.4358 300.6750 0269345 357.2226 2.7774 13.40896756 01
| Epoch (UTC): | 25 September 2023 23:49:43 |
| Eccentricity: | 0.0269345 |
| inclination: | 63.4358° |
| perigee height: | 904 km |
| apogee height: | 1307 km |
| right ascension of ascending node: | 300.6750° |
| argument of perigee: | 357.2226° |
| revolutions per day: | 13.40896756 |
| mean anomaly at epoch: | 2.7774° |
| 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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