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 61758U 26145.58979229 +.00000000 +00000-0 +19280-3 0 00002
2 61758 97.3260 346.5643 0007211 131.6214 228.5628 14.97815754 00
| Epoch (UTC): | 25 May 2026 14:09:18 |
| Eccentricity: | 0.0007211 |
| inclination: | 97.3260° |
| perigee height: | 569 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 346.5643° |
| argument of perigee: | 131.6214° |
| revolutions per day: | 14.97815754 |
| mean anomaly at epoch: | 228.5628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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