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 66744U 26144.77586562 +.00000000 +00000-0 +94015-4 0 00006
2 66744 97.4211 218.5488 0004521 87.8940 272.2812 15.18224402 00
| Epoch (UTC): | 24 May 2026 18:37:14 |
| Eccentricity: | 0.0004521 |
| inclination: | 97.4211° |
| perigee height: | 508 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 218.5488° |
| argument of perigee: | 87.8940° |
| revolutions per day: | 15.18224402 |
| mean anomaly at epoch: | 272.2812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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