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 41890U 26145.36147492 +.00000000 +00000-0 +34298-3 0 00008
2 41890 34.9462 21.3763 0008238 330.2498 29.7758 15.58762032 01
| Epoch (UTC): | 25 May 2026 08:40:31 |
| Eccentricity: | 0.0008238 |
| inclination: | 34.9462° |
| perigee height: | 386 km |
| apogee height: | 397 km |
| right ascension of ascending node: | 21.3763° |
| argument of perigee: | 330.2498° |
| revolutions per day: | 15.58762032 |
| mean anomaly at epoch: | 29.7758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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