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 62313U 26145.34901851 +.00000000 +00000-0 +66541-3 0 00002
2 62313 53.1572 184.8628 0000870 95.9224 264.1876 15.30204846 00
| Epoch (UTC): | 25 May 2026 08:22:35 |
| Eccentricity: | 0.0000870 |
| inclination: | 53.1572° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.8628° |
| argument of perigee: | 95.9224° |
| revolutions per day: | 15.30204846 |
| mean anomaly at epoch: | 264.1876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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