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 37154U 26145.58149272 +.00000000 +00000-0 +39862-4 0 00001
2 37154 82.4607 76.3918 0015072 2.4607 171.0266 12.43746698 00
| Epoch (UTC): | 25 May 2026 13:57:20 |
| Eccentricity: | 0.0015072 |
| inclination: | 82.4607° |
| perigee height: | 1479 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 76.3918° |
| argument of perigee: | 2.4607° |
| revolutions per day: | 12.43746698 |
| mean anomaly at epoch: | 171.0266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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