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 62727U 26145.61689462 +.00000000 +00000-0 +40947-3 0 00004
2 62727 97.4265 221.2340 0006645 357.6386 2.4820 15.26969545 00
| Epoch (UTC): | 25 May 2026 14:48:19 |
| Eccentricity: | 0.0006645 |
| inclination: | 97.4265° |
| perigee height: | 480 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 221.2340° |
| argument of perigee: | 357.6386° |
| revolutions per day: | 15.26969545 |
| mean anomaly at epoch: | 2.4820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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