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 27607U 02058C 22221.50250547 .00000433 00000-0 79795-4 0 9995
2 27607 64.5548 139.5561 0080590 284.2563 74.9599 14.76193962 56202
| Epoch (UTC): | 09 August 2022 12:03:36 |
| Eccentricity: | 0.0080590 |
| inclination: | 64.5548° |
| perigee height: | 585 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 139.5561° |
| argument of perigee: | 284.2563° |
| revolutions per day: | 14.76193962 |
| mean anomaly at epoch: | 74.9599° |
| orbit number at epoch: | 5620 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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