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 67537U 26145.42941419 +.00000000 +00000-0 +41867-3 0 00002
2 67537 97.2876 32.4652 0001063 96.6150 263.5213 15.33449678 00
| Epoch (UTC): | 25 May 2026 10:18:21 |
| Eccentricity: | 0.0001063 |
| inclination: | 97.2876° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 32.4652° |
| argument of perigee: | 96.6150° |
| revolutions per day: | 15.33449678 |
| mean anomaly at epoch: | 263.5213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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