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 64900U 26145.54459050 +.00000000 +00000-0 +21499-3 0 00000
2 64900 97.4327 224.5634 0000661 155.1804 204.9463 15.20209754 09
| Epoch (UTC): | 25 May 2026 13:04:12 |
| Eccentricity: | 0.0000661 |
| inclination: | 97.4327° |
| perigee height: | 505 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 224.5634° |
| argument of perigee: | 155.1804° |
| revolutions per day: | 15.20209754 |
| mean anomaly at epoch: | 204.9463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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