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 26064.68200080 +.00000000 +00000-0 +14903-3 0 00001
2 27601 98.3197 25.2003 0070259 172.5597 3.6810 14.33757734 08
| Epoch (UTC): | 05 March 2026 16:22:04 |
| Eccentricity: | 0.0070259 |
| inclination: | 98.3197° |
| perigee height: | 729 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 25.2003° |
| argument of perigee: | 172.5597° |
| revolutions per day: | 14.33757734 |
| mean anomaly at epoch: | 3.6810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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