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 65194U 26145.37288102 +.00000000 +00000-0 +26906-3 0 00003
2 65194 97.4473 17.9311 0002525 89.9878 270.1639 15.05656828 00
| Epoch (UTC): | 25 May 2026 08:56:56 |
| Eccentricity: | 0.0002525 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.9311° |
| argument of perigee: | 89.9878° |
| revolutions per day: | 15.05656828 |
| mean anomaly at epoch: | 270.1639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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