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 68774U 26145.58335647 +.00000000 +00000-0 -23576-1 0 00009
2 68774 97.2848 182.4444 0001672 85.8843 62.3048 15.62390927 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001672 |
| inclination: | 97.2848° |
| perigee height: | 380 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 182.4444° |
| argument of perigee: | 85.8843° |
| revolutions per day: | 15.62390927 |
| mean anomaly at epoch: | 62.3048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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