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 65481U 26145.35305296 +.00000000 +00000-0 +81179-3 0 00007
2 65481 53.1568 261.9100 0000554 84.9890 275.1176 15.34417788 02
| Epoch (UTC): | 25 May 2026 08:28:23 |
| Eccentricity: | 0.0000554 |
| inclination: | 53.1568° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 261.9100° |
| argument of perigee: | 84.9890° |
| revolutions per day: | 15.34417788 |
| mean anomaly at epoch: | 275.1176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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