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 61774U 26145.60433955 +.00000000 +00000-0 +64575-3 0 00001
2 61774 97.2928 21.5444 0007105 33.0094 327.1604 15.57952877 05
| Epoch (UTC): | 25 May 2026 14:30:14 |
| Eccentricity: | 0.0007105 |
| inclination: | 97.2928° |
| perigee height: | 389 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 21.5444° |
| argument of perigee: | 33.0094° |
| revolutions per day: | 15.57952877 |
| mean anomaly at epoch: | 327.1604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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