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 37188U 26145.51207167 +.00000000 +00000-0 +53860-4 0 00003
2 37188 52.0012 177.6969 0000165 294.4169 228.9361 12.62265838 05
| Epoch (UTC): | 25 May 2026 12:17:22 |
| Eccentricity: | 0.0000165 |
| inclination: | 52.0012° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 177.6969° |
| argument of perigee: | 294.4169° |
| revolutions per day: | 12.62265838 |
| mean anomaly at epoch: | 228.9361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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