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 62797U 26145.59164596 +.00000000 +00000-0 +13352-3 0 00004
2 62797 88.9727 86.0496 0012921 227.9478 132.0575 13.51013728 05
| Epoch (UTC): | 25 May 2026 14:11:58 |
| Eccentricity: | 0.0012921 |
| inclination: | 88.9727° |
| perigee height: | 1059 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 86.0496° |
| argument of perigee: | 227.9478° |
| revolutions per day: | 13.51013728 |
| mean anomaly at epoch: | 132.0575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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