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 65368U 26145.48375728 +.00000000 +00000-0 +10585-2 0 00004
2 65368 53.1583 171.4114 0001587 90.2751 269.8433 15.34379580 09
| Epoch (UTC): | 25 May 2026 11:36:36 |
| Eccentricity: | 0.0001587 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 171.4114° |
| argument of perigee: | 90.2751° |
| revolutions per day: | 15.34379580 |
| mean anomaly at epoch: | 269.8433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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