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 44883U 26145.60031791 +.00000000 +00000-0 +11246-3 0 00002
2 44883 97.7500 213.5618 0000357 203.1755 156.9442 14.81612663 00
| Epoch (UTC): | 25 May 2026 14:24:27 |
| Eccentricity: | 0.0000357 |
| inclination: | 97.7500° |
| perigee height: | 624 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 213.5618° |
| argument of perigee: | 203.1755° |
| revolutions per day: | 14.81612663 |
| mean anomaly at epoch: | 156.9442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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