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 62986U 26145.03124453 +.00000000 +00000-0 +18469-2 0 00004
2 62986 42.9992 260.8768 0001139 299.2805 60.7948 15.70912554 07
| Epoch (UTC): | 25 May 2026 00:44:59 |
| Eccentricity: | 0.0001139 |
| inclination: | 42.9992° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 260.8768° |
| argument of perigee: | 299.2805° |
| revolutions per day: | 15.70912554 |
| mean anomaly at epoch: | 60.7948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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