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 64153U 26145.41167206 +.00000000 +00000-0 +33846-3 0 00004
2 64153 97.4458 196.7831 0001943 114.9684 245.1745 15.05657394 06
| Epoch (UTC): | 25 May 2026 09:52:48 |
| Eccentricity: | 0.0001943 |
| inclination: | 97.4458° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 196.7831° |
| argument of perigee: | 114.9684° |
| revolutions per day: | 15.05657394 |
| mean anomaly at epoch: | 245.1745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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