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 64670U 26145.22077259 +.00000000 +00000-0 +75296-3 0 00000
2 64670 53.1599 130.6933 0003235 95.9370 264.2002 15.34419781 07
| Epoch (UTC): | 25 May 2026 05:17:54 |
| Eccentricity: | 0.0003235 |
| inclination: | 53.1599° |
| perigee height: | 460 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 130.6933° |
| argument of perigee: | 95.9370° |
| revolutions per day: | 15.34419781 |
| mean anomaly at epoch: | 264.2002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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