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 26073.96702707 +.00000000 +00000-0 +31810-3 0 00005
2 27939 98.3445 255.6750 0010752 202.2227 306.9819 14.73272902 00
| Epoch (UTC): | 14 March 2026 23:12:31 |
| Eccentricity: | 0.0010752 |
| inclination: | 98.3445° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 255.6750° |
| argument of perigee: | 202.2227° |
| revolutions per day: | 14.73272902 |
| mean anomaly at epoch: | 306.9819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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