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 37744U 26145.63092258 +.00000000 +00000-0 +20763-4 0 00003
2 37744 51.9920 218.4839 0000565 110.1106 53.5404 12.62266555 05
| Epoch (UTC): | 25 May 2026 15:08:31 |
| Eccentricity: | 0.0000565 |
| inclination: | 51.9920° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 218.4839° |
| argument of perigee: | 110.1106° |
| revolutions per day: | 12.62266555 |
| mean anomaly at epoch: | 53.5404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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