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 66768U 26145.15406174 +.00000000 +00000-0 +25844-3 0 00008
2 66768 97.4154 219.2804 0001324 127.4540 232.6816 15.20755166 00
| Epoch (UTC): | 25 May 2026 03:41:50 |
| Eccentricity: | 0.0001324 |
| inclination: | 97.4154° |
| perigee height: | 503 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 219.2804° |
| argument of perigee: | 127.4540° |
| revolutions per day: | 15.20755166 |
| mean anomaly at epoch: | 232.6816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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