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 26039.18714053 +.00000000 +00000-0 +20037-3 0 00007
2 27939 98.3405 219.9334 0010697 322.9809 158.6130 14.73166390 02
| Epoch (UTC): | 08 February 2026 04:29:28 |
| Eccentricity: | 0.0010697 |
| inclination: | 98.3405° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 219.9334° |
| argument of perigee: | 322.9809° |
| revolutions per day: | 14.73166390 |
| mean anomaly at epoch: | 158.6130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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