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 65542U 26145.62742634 +.00000000 +00000-0 +25978-3 0 00001
2 65542 97.4456 215.1973 0001174 131.6772 228.4556 15.05656940 00
| Epoch (UTC): | 25 May 2026 15:03:29 |
| Eccentricity: | 0.0001174 |
| inclination: | 97.4456° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 215.1973° |
| argument of perigee: | 131.6772° |
| revolutions per day: | 15.05656940 |
| mean anomaly at epoch: | 228.4556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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