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 60026U 26145.09210947 +.00000000 +00000-0 +85639-4 0 00002
2 60026 53.1604 80.5598 0001237 85.1062 275.0080 15.30204772 08
| Epoch (UTC): | 25 May 2026 02:12:38 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.5598° |
| argument of perigee: | 85.1062° |
| revolutions per day: | 15.30204772 |
| mean anomaly at epoch: | 275.0080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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