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 61745U 26145.62872883 +.00000000 +00000-0 +65784-3 0 00001
2 61745 97.2998 22.7020 0005218 19.7885 340.3573 15.59019358 07
| Epoch (UTC): | 25 May 2026 15:05:22 |
| Eccentricity: | 0.0005218 |
| inclination: | 97.2998° |
| perigee height: | 387 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 22.7020° |
| argument of perigee: | 19.7885° |
| revolutions per day: | 15.59019358 |
| mean anomaly at epoch: | 340.3573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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