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 65672U 26145.63119412 +.00000000 +00000-0 +43225-3 0 00003
2 65672 97.4457 189.5965 0002133 127.0747 233.0676 15.05659028 02
| Epoch (UTC): | 25 May 2026 15:08:55 |
| Eccentricity: | 0.0002133 |
| inclination: | 97.4457° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5965° |
| argument of perigee: | 127.0747° |
| revolutions per day: | 15.05659028 |
| mean anomaly at epoch: | 233.0676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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