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 65195U 26145.37567029 +.00000000 +00000-0 +51798-3 0 00009
2 65195 97.4479 17.9266 0002673 85.2074 274.9458 15.05657766 00
| Epoch (UTC): | 25 May 2026 09:00:57 |
| Eccentricity: | 0.0002673 |
| inclination: | 97.4479° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.9266° |
| argument of perigee: | 85.2074° |
| revolutions per day: | 15.05657766 |
| mean anomaly at epoch: | 274.9458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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