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 68276U 26145.58335647 +.00000000 +00000-0 -59829-4 0 00009
2 68276 53.1599 321.1446 0001133 94.9335 31.6215 15.34393684 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001133 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 321.1446° |
| argument of perigee: | 94.9335° |
| revolutions per day: | 15.34393684 |
| mean anomaly at epoch: | 31.6215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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