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 22138.44400316 .00001163 00000-0 18071-3 0 9996
2 27607 64.5564 33.7319 0076705 300.3185 59.0345 14.76087231 43940
| Epoch (UTC): | 18 May 2022 10:39:21 |
| Eccentricity: | 0.0076705 |
| inclination: | 64.5564° |
| perigee height: | 588 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 33.7319° |
| argument of perigee: | 300.3185° |
| revolutions per day: | 14.76087231 |
| mean anomaly at epoch: | 59.0345° |
| orbit number at epoch: | 4394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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