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 42969U 26145.36438377 +.00000000 +00000-0 +41856-4 0 00000
2 42969 98.7918 87.6593 0001074 77.6951 282.4345 14.19514481 05
| Epoch (UTC): | 25 May 2026 08:44:42 |
| Eccentricity: | 0.0001074 |
| inclination: | 98.7918° |
| perigee height: | 826 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 87.6593° |
| argument of perigee: | 77.6951° |
| revolutions per day: | 14.19514481 |
| mean anomaly at epoch: | 282.4345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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