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 65367U 26145.58335647 +.00000000 +00000-0 +25436-2 0 00001
2 65367 53.1592 171.0128 0000462 179.0010 336.8677 15.34317134 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000462 |
| inclination: | 53.1592° |
| perigee height: | 463 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 171.0128° |
| argument of perigee: | 179.0010° |
| revolutions per day: | 15.34317134 |
| mean anomaly at epoch: | 336.8677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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