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 27939U 26145.53502464 +.00000000 +00000-0 +65031-4 0 00009
2 27939 98.3476 329.2551 0010985 347.4988 97.1452 14.73418651 00
| Epoch (UTC): | 25 May 2026 12:50:26 |
| Eccentricity: | 0.0010985 |
| inclination: | 98.3476° |
| perigee height: | 642 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 329.2551° |
| argument of perigee: | 347.4988° |
| revolutions per day: | 14.73418651 |
| mean anomaly at epoch: | 97.1452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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