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 41896U 26144.67728949 +.00000000 +00000-0 +18995-2 0 00004
2 41896 31.9400 17.6224 6992782 33.1321 355.6610 2.57649789 08
| Epoch (UTC): | 24 May 2026 16:15:17 |
| Eccentricity: | 0.6992782 |
| inclination: | 31.9400° |
| perigee height: | 381 km |
| apogee height: | 31815 km |
| right ascension of ascending node: | 17.6224° |
| argument of perigee: | 33.1321° |
| revolutions per day: | 2.57649789 |
| mean anomaly at epoch: | 355.6610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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