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 67865U 26145.55922667 +.00000000 +00000-0 +32990-3 0 00001
2 67865 53.1603 207.2720 0001042 70.3158 289.7955 15.30203099 00
| Epoch (UTC): | 25 May 2026 13:25:17 |
| Eccentricity: | 0.0001042 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.2720° |
| argument of perigee: | 70.3158° |
| revolutions per day: | 15.30203099 |
| mean anomaly at epoch: | 289.7955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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