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 44907U 26145.56469080 +.00000000 +00000-0 +21884-3 0 00009
2 44907 82.5180 98.0854 0009618 269.6721 90.3257 12.42891066 06
| Epoch (UTC): | 25 May 2026 13:33:09 |
| Eccentricity: | 0.0009618 |
| inclination: | 82.5180° |
| perigee height: | 1487 km |
| apogee height: | 1502 km |
| right ascension of ascending node: | 98.0854° |
| argument of perigee: | 269.6721° |
| revolutions per day: | 12.42891066 |
| mean anomaly at epoch: | 90.3257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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