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 65401U 26145.39921123 +.00000000 +00000-0 +24070-3 0 00003
2 65401 97.4477 16.7806 0001666 86.6268 273.5150 15.05659421 00
| Epoch (UTC): | 25 May 2026 09:34:51 |
| Eccentricity: | 0.0001666 |
| inclination: | 97.4477° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.7806° |
| argument of perigee: | 86.6268° |
| revolutions per day: | 15.05659421 |
| mean anomaly at epoch: | 273.5150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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