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 61678U 26145.23887323 +.00000000 +00000-0 +13172-4 0 00003
2 61678 53.1607 94.2392 0001258 94.8463 265.2683 15.34386588 04
| Epoch (UTC): | 25 May 2026 05:43:58 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 94.2392° |
| argument of perigee: | 94.8463° |
| revolutions per day: | 15.34386588 |
| mean anomaly at epoch: | 265.2683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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