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 41787U 26087.88989956 +.00000000 +00000-0 +16360-3 0 00004
2 41787 97.8181 90.7932 0029953 101.7451 258.7117 14.67551852 05
| Epoch (UTC): | 28 March 2026 21:21:27 |
| Eccentricity: | 0.0029953 |
| inclination: | 97.8181° |
| perigee height: | 648 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 90.7932° |
| argument of perigee: | 101.7451° |
| revolutions per day: | 14.67551852 |
| mean anomaly at epoch: | 258.7117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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