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 62276U 26145.50446257 +.00000000 +00000-0 +18088-2 0 00004
2 62276 42.9982 313.5573 0001617 264.9723 95.0960 15.70921487 07
| Epoch (UTC): | 25 May 2026 12:06:25 |
| Eccentricity: | 0.0001617 |
| inclination: | 42.9982° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 313.5573° |
| argument of perigee: | 264.9723° |
| revolutions per day: | 15.70921487 |
| mean anomaly at epoch: | 95.0960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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