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 26071.71513296 +.00000000 +00000-0 +25268-3 0 00009
2 27939 98.3446 253.3603 0010643 209.8126 243.0179 14.73264890 00
| Epoch (UTC): | 12 March 2026 17:09:47 |
| Eccentricity: | 0.0010643 |
| inclination: | 98.3446° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 253.3603° |
| argument of perigee: | 209.8126° |
| revolutions per day: | 14.73264890 |
| mean anomaly at epoch: | 243.0179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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