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 65399U 26145.60965933 +.00000000 +00000-0 +20754-3 0 00005
2 65399 97.4490 16.9567 0001719 82.3741 277.7682 15.05658223 00
| Epoch (UTC): | 25 May 2026 14:37:54 |
| Eccentricity: | 0.0001719 |
| inclination: | 97.4490° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9567° |
| argument of perigee: | 82.3741° |
| revolutions per day: | 15.05658223 |
| mean anomaly at epoch: | 277.7682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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