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 67678U 26145.60363199 +.00000000 +00000-0 +42056-3 0 00002
2 67678 96.6222 209.6446 0017584 207.5920 152.4389 15.24794618 03
| Epoch (UTC): | 25 May 2026 14:29:13 |
| Eccentricity: | 0.0017584 |
| inclination: | 96.6222° |
| perigee height: | 479 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 209.6446° |
| argument of perigee: | 207.5920° |
| revolutions per day: | 15.24794618 |
| mean anomaly at epoch: | 152.4389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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