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 27940U 26041.45516822 +.00000000 +00000-0 +14763-3 0 00005
2 27940 98.3776 216.0969 0013743 40.5090 319.7135 14.69321784 07
| Epoch (UTC): | 10 February 2026 10:55:26 |
| Eccentricity: | 0.0013743 |
| inclination: | 98.3776° |
| perigee height: | 654 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 216.0969° |
| argument of perigee: | 40.5090° |
| revolutions per day: | 14.69321784 |
| mean anomaly at epoch: | 319.7135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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