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 37730U 26145.53191671 +.00000000 +00000-0 +85242-4 0 00009
2 37730 97.9323 110.3907 0009616 101.6311 35.2236 14.64307471 09
| Epoch (UTC): | 25 May 2026 12:45:57 |
| Eccentricity: | 0.0009616 |
| inclination: | 97.9323° |
| perigee height: | 673 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 110.3907° |
| argument of perigee: | 101.6311° |
| revolutions per day: | 14.64307471 |
| mean anomaly at epoch: | 35.2236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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