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 58262U 26145.24166906 +.00000000 +00000-0 +37057-3 0 00003
2 58262 97.3927 242.2528 0005308 174.1142 186.0179 15.61525237 02
| Epoch (UTC): | 25 May 2026 05:48:00 |
| Eccentricity: | 0.0005308 |
| inclination: | 97.3927° |
| perigee height: | 380 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 242.2528° |
| argument of perigee: | 174.1142° |
| revolutions per day: | 15.61525237 |
| mean anomaly at epoch: | 186.0179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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