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 61737U 26145.63923844 +.00000000 +00000-0 +28222-3 0 00003
2 61737 97.3254 346.3747 0008192 131.4382 228.7546 14.97462239 03
| Epoch (UTC): | 25 May 2026 15:20:30 |
| Eccentricity: | 0.0008192 |
| inclination: | 97.3254° |
| perigee height: | 569 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 346.3747° |
| argument of perigee: | 131.4382° |
| revolutions per day: | 14.97462239 |
| mean anomaly at epoch: | 228.7546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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