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 62912U 26145.60573608 +.00000000 +00000-0 +14827-2 0 00000
2 62912 43.0033 243.6227 0002518 264.2322 95.8259 15.70868151 08
| Epoch (UTC): | 25 May 2026 14:32:15 |
| Eccentricity: | 0.0002518 |
| inclination: | 43.0033° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 243.6227° |
| argument of perigee: | 264.2322° |
| revolutions per day: | 15.70868151 |
| mean anomaly at epoch: | 95.8259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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