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 41899U 26145.45656433 +.00000000 +00000-0 +11803-3 0 00004
2 41899 98.5374 142.6525 0021409 22.7124 337.5018 14.60732237 00
| Epoch (UTC): | 25 May 2026 10:57:27 |
| Eccentricity: | 0.0021409 |
| inclination: | 98.5374° |
| perigee height: | 676 km |
| apogee height: | 706 km |
| right ascension of ascending node: | 142.6525° |
| argument of perigee: | 22.7124° |
| revolutions per day: | 14.60732237 |
| mean anomaly at epoch: | 337.5018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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