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 65276U 26145.60132509 +.00000000 +00000-0 +20831-3 0 00000
2 65276 97.4462 198.0932 0002930 127.6535 232.4959 15.05656588 08
| Epoch (UTC): | 25 May 2026 14:25:54 |
| Eccentricity: | 0.0002930 |
| inclination: | 97.4462° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 198.0932° |
| argument of perigee: | 127.6535° |
| revolutions per day: | 15.05656588 |
| mean anomaly at epoch: | 232.4959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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