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 56964U 26145.58057027 +.00000000 +00000-0 +16420-3 0 00001
2 56964 97.6238 281.7358 0011790 63.3478 296.8967 15.28329337 00
| Epoch (UTC): | 25 May 2026 13:56:01 |
| Eccentricity: | 0.0011790 |
| inclination: | 97.6238° |
| perigee height: | 473 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 281.7358° |
| argument of perigee: | 63.3478° |
| revolutions per day: | 15.28329337 |
| mean anomaly at epoch: | 296.8967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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