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 62903U 26145.73272492 +.00000000 +00000-0 +99654-4 0 00004
2 62903 81.9948 97.4075 0011319 124.8050 235.4236 14.94923051 01
| Epoch (UTC): | 25 May 2026 17:35:07 |
| Eccentricity: | 0.0011319 |
| inclination: | 81.9948° |
| perigee height: | 575 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 97.4075° |
| argument of perigee: | 124.8050° |
| revolutions per day: | 14.94923051 |
| mean anomaly at epoch: | 235.4236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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