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 26069.96215992 +.00000000 +00000-0 +32416-3 0 00008
2 27939 98.3442 251.5585 0010514 215.7887 305.2840 14.73260539 04
| Epoch (UTC): | 10 March 2026 23:05:30 |
| Eccentricity: | 0.0010514 |
| inclination: | 98.3442° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 251.5585° |
| argument of perigee: | 215.7887° |
| revolutions per day: | 14.73260539 |
| mean anomaly at epoch: | 305.2840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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