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 37788U 26150.61943596 +.00000000 +00000-0 +16610-3 0 00000
2 37788 98.2717 47.8407 0034403 174.6778 253.1919 14.76489503 00
| Epoch (UTC): | 30 May 2026 14:51:59 |
| Eccentricity: | 0.0034403 |
| inclination: | 98.2717° |
| perigee height: | 616 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 47.8407° |
| argument of perigee: | 174.6778° |
| revolutions per day: | 14.76489503 |
| mean anomaly at epoch: | 253.1919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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