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 64158U 26145.38121326 +.00000000 +00000-0 +30845-3 0 00004
2 64158 97.4503 196.6774 0001544 99.6406 260.4996 15.05648028 07
| Epoch (UTC): | 25 May 2026 09:08:56 |
| Eccentricity: | 0.0001544 |
| inclination: | 97.4503° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.6774° |
| argument of perigee: | 99.6406° |
| revolutions per day: | 15.05648028 |
| mean anomaly at epoch: | 260.4996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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