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 62610U 26145.18699451 +.00000000 +00000-0 +41321-3 0 00003
2 62610 97.4003 227.7428 0005986 45.8761 314.2972 15.30977110 03
| Epoch (UTC): | 25 May 2026 04:29:16 |
| Eccentricity: | 0.0005986 |
| inclination: | 97.4003° |
| perigee height: | 469 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 227.7428° |
| argument of perigee: | 45.8761° |
| revolutions per day: | 15.30977110 |
| mean anomaly at epoch: | 314.2972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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