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 65190U 26145.58335647 +.00000000 +00000-0 +36732-2 0 00006
2 65190 97.4458 18.0908 0002575 71.7166 243.5821 15.05630609 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002575 |
| inclination: | 97.4458° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0908° |
| argument of perigee: | 71.7166° |
| revolutions per day: | 15.05630609 |
| mean anomaly at epoch: | 243.5821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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