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 27941U 26088.10972948 +.00000000 +00000-0 +19680-3 0 00007
2 27941 98.0066 278.8526 0042151 191.3739 168.6530 14.90094640 04
| Epoch (UTC): | 29 March 2026 02:38:00 |
| Eccentricity: | 0.0042151 |
| inclination: | 98.0066° |
| perigee height: | 568 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 278.8526° |
| argument of perigee: | 191.3739° |
| revolutions per day: | 14.90094640 |
| mean anomaly at epoch: | 168.6530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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