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 64940U 26145.57031187 +.00000000 +00000-0 +21698-3 0 00005
2 64940 97.4520 9.8156 0001818 87.3835 272.7600 15.04844521 01
| Epoch (UTC): | 25 May 2026 13:41:14 |
| Eccentricity: | 0.0001818 |
| inclination: | 97.4520° |
| perigee height: | 551 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 9.8156° |
| argument of perigee: | 87.3835° |
| revolutions per day: | 15.04844521 |
| mean anomaly at epoch: | 272.7600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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