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 65393U 26145.14721972 +.00000000 +00000-0 +23843-3 0 00003
2 65393 97.4506 16.5019 0001720 74.3981 285.7436 15.05659999 06
| Epoch (UTC): | 25 May 2026 03:31:59 |
| Eccentricity: | 0.0001720 |
| inclination: | 97.4506° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.5019° |
| argument of perigee: | 74.3981° |
| revolutions per day: | 15.05659999 |
| mean anomaly at epoch: | 285.7436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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