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 65193U 26145.11812065 +.00000000 +00000-0 +28471-3 0 00004
2 65193 97.4532 17.6614 0002027 83.6329 276.5129 15.05658214 02
| Epoch (UTC): | 25 May 2026 02:50:05 |
| Eccentricity: | 0.0002027 |
| inclination: | 97.4532° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.6614° |
| argument of perigee: | 83.6329° |
| revolutions per day: | 15.05658214 |
| mean anomaly at epoch: | 276.5129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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