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 62098U 26145.53850213 +.00000000 +00000-0 +12213-2 0 00004
2 62098 43.0060 299.4825 0002686 264.8566 95.1995 15.70923033 09
| Epoch (UTC): | 25 May 2026 12:55:26 |
| Eccentricity: | 0.0002686 |
| inclination: | 43.0060° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 299.4825° |
| argument of perigee: | 264.8566° |
| revolutions per day: | 15.70923033 |
| mean anomaly at epoch: | 95.1995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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