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 66298U 26145.58723727 +.00000000 +00000-0 +13436-3 0 00003
2 66298 45.3812 241.0659 0014054 265.1156 94.8125 15.20742084 05
| Epoch (UTC): | 25 May 2026 14:05:37 |
| Eccentricity: | 0.0014054 |
| inclination: | 45.3812° |
| perigee height: | 494 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 241.0659° |
| argument of perigee: | 265.1156° |
| revolutions per day: | 15.20742084 |
| mean anomaly at epoch: | 94.8125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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