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 27445U 26145.46929316 +.00000000 +00000-0 +00000-0 0 00003
2 27445 3.6739 78.2772 0001780 27.6420 211.2218 1.00271429 05
| Epoch (UTC): | 25 May 2026 11:15:46 |
| Eccentricity: | 0.0001780 |
| inclination: | 3.6739° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 78.2772° |
| argument of perigee: | 27.6420° |
| revolutions per day: | 1.00271429 |
| mean anomaly at epoch: | 211.2218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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