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 44390U 26145.62013520 +.00000000 +00000-0 +43637-3 0 00006
2 44390 97.8781 177.2133 0013861 31.4601 328.7464 15.28702290 00
| Epoch (UTC): | 25 May 2026 14:52:59 |
| Eccentricity: | 0.0013861 |
| inclination: | 97.8781° |
| perigee height: | 470 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 177.2133° |
| argument of perigee: | 31.4601° |
| revolutions per day: | 15.28702290 |
| mean anomaly at epoch: | 328.7464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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