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 27601U 26087.88908954 +.00000000 +00000-0 +12554-3 0 00003
2 27601 98.3234 47.5275 0071365 104.1133 267.6834 14.33773303 02
| Epoch (UTC): | 28 March 2026 21:20:17 |
| Eccentricity: | 0.0071365 |
| inclination: | 98.3234° |
| perigee height: | 728 km |
| apogee height: | 830 km |
| right ascension of ascending node: | 47.5275° |
| argument of perigee: | 104.1133° |
| revolutions per day: | 14.33773303 |
| mean anomaly at epoch: | 267.6834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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