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 41853U 26145.60113462 +.00000000 +00000-0 +28465-3 0 00003
2 41853 98.0592 11.3142 0006473 129.4010 230.7800 15.24268604 03
| Epoch (UTC): | 25 May 2026 14:25:38 |
| Eccentricity: | 0.0006473 |
| inclination: | 98.0592° |
| perigee height: | 489 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 11.3142° |
| argument of perigee: | 129.4010° |
| revolutions per day: | 15.24268604 |
| mean anomaly at epoch: | 230.7800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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