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 64860U 26145.31353382 +.00000000 +00000-0 +21186-3 0 00004
2 64860 97.4474 0.6072 0002645 90.7415 269.4116 15.05658331 05
| Epoch (UTC): | 25 May 2026 07:31:29 |
| Eccentricity: | 0.0002645 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.6072° |
| argument of perigee: | 90.7415° |
| revolutions per day: | 15.05658331 |
| mean anomaly at epoch: | 269.4116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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