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 40617U 26145.52276507 +.00000000 +00000-0 +00000-0 0 00003
2 40617 0.0510 90.8953 0003063 331.0404 61.3874 1.00273734 03
| Epoch (UTC): | 25 May 2026 12:32:46 |
| Eccentricity: | 0.0003063 |
| inclination: | 0.0510° |
| perigee height: | 35773 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 90.8953° |
| argument of perigee: | 331.0404° |
| revolutions per day: | 1.00273734 |
| mean anomaly at epoch: | 61.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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