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 62836U 26145.52243757 +.00000000 +00000-0 +76850-3 0 00000
2 62836 43.0013 202.9392 0001347 267.7481 92.3232 15.70861489 05
| Epoch (UTC): | 25 May 2026 12:32:18 |
| Eccentricity: | 0.0001347 |
| inclination: | 43.0013° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 202.9392° |
| argument of perigee: | 267.7481° |
| revolutions per day: | 15.70861489 |
| mean anomaly at epoch: | 92.3232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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