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 65141U 26145.41159522 +.00000000 +00000-0 +86133-4 0 00002
2 65141 51.8975 191.2966 0000333 87.1890 272.9111 14.79933132 05
| Epoch (UTC): | 25 May 2026 09:52:41 |
| Eccentricity: | 0.0000333 |
| inclination: | 51.8975° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 191.2966° |
| argument of perigee: | 87.1890° |
| revolutions per day: | 14.79933132 |
| mean anomaly at epoch: | 272.9111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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