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 61851U 26145.48463860 +.00000000 +00000-0 +11093-5 0 00000
2 61851 43.0025 152.9397 0001640 258.7707 101.2961 15.27575455 06
| Epoch (UTC): | 25 May 2026 11:37:52 |
| Eccentricity: | 0.0001640 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 152.9397° |
| argument of perigee: | 258.7707° |
| revolutions per day: | 15.27575455 |
| mean anomaly at epoch: | 101.2961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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