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 37222U 10062A 23285.76578231 0.00001400 00000-0 18628-3 0 00
2 37222 71.9710 175.1774 0017676 156.5668 203.4331 14.79553733 02
| Epoch (UTC): | 12 October 2023 18:22:43 |
| Eccentricity: | 0.0017676 |
| inclination: | 71.9710° |
| perigee height: | 618 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 175.1774° |
| argument of perigee: | 156.5668° |
| revolutions per day: | 14.79553733 |
| mean anomaly at epoch: | 203.4331° |
| 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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