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 67261U 26145.12758507 +.00000000 +00000-0 +69485-3 0 00003
2 67261 97.3975 220.5288 0015193 85.4185 274.8788 15.25476289 04
| Epoch (UTC): | 25 May 2026 03:03:43 |
| Eccentricity: | 0.0015193 |
| inclination: | 97.3975° |
| perigee height: | 479 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 220.5288° |
| argument of perigee: | 85.4185° |
| revolutions per day: | 15.25476289 |
| mean anomaly at epoch: | 274.8788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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