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 is defined by the following mean orbital elements,
1 27607U 26076.17109669 +.00000000 +00000-0 +18763-3 0 00003
2 27607 64.5530 53.6327 0075344 279.3221 79.9371 14.82815203 02
| Epoch (UTC): | 17 March 2026 04:06:22 |
| Eccentricity: | 0.0075344 |
| inclination: | 64.5530° |
| perigee height: | 568 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 53.6327° |
| argument of perigee: | 279.3221° |
| revolutions per day: | 14.82815203 |
| mean anomaly at epoch: | 79.9371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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