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 37216U 26145.49015632 +.00000000 +00000-0 +52016-4 0 00008
2 37216 97.8893 329.4193 0001404 87.7263 272.4111 14.82162725 04
| Epoch (UTC): | 25 May 2026 11:45:49 |
| Eccentricity: | 0.0001404 |
| inclination: | 97.8893° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 329.4193° |
| argument of perigee: | 87.7263° |
| revolutions per day: | 14.82162725 |
| mean anomaly at epoch: | 272.4111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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