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 46144U 26145.58335647 +.00000000 +00000-0 +86734-3 0 00002
2 46144 53.0362 234.2607 0007340 328.3748 235.5172 15.84146446 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007340 |
| inclination: | 53.0362° |
| perigee height: | 314 km |
| apogee height: | 324 km |
| right ascension of ascending node: | 234.2607° |
| argument of perigee: | 328.3748° |
| revolutions per day: | 15.84146446 |
| mean anomaly at epoch: | 235.5172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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