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 44408U 26145.10319247 +.00000000 +00000-0 +42789-3 0 00001
2 44408 97.6778 188.4108 0009792 102.2108 258.0247 15.64476898 03
| Epoch (UTC): | 25 May 2026 02:28:35 |
| Eccentricity: | 0.0009792 |
| inclination: | 97.6778° |
| perigee height: | 368 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 188.4108° |
| argument of perigee: | 102.2108° |
| revolutions per day: | 15.64476898 |
| mean anomaly at epoch: | 258.0247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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