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 41857U 26145.60858693 +.00000000 +00000-0 +10926-3 0 00002
2 41857 98.5843 156.8262 0006495 97.4419 262.7503 14.32688110 01
| Epoch (UTC): | 25 May 2026 14:36:21 |
| Eccentricity: | 0.0006495 |
| inclination: | 98.5843° |
| perigee height: | 778 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 156.8262° |
| argument of perigee: | 97.4419° |
| revolutions per day: | 14.32688110 |
| mean anomaly at epoch: | 262.7503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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