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 37189U 26145.34699602 +.00000000 +00000-0 +55954-4 0 00000
2 37189 51.9989 177.4684 0000164 93.0665 279.8151 12.62268273 00
| Epoch (UTC): | 25 May 2026 08:19:40 |
| Eccentricity: | 0.0000164 |
| inclination: | 51.9989° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 177.4684° |
| argument of perigee: | 93.0665° |
| revolutions per day: | 12.62268273 |
| mean anomaly at epoch: | 279.8151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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