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 48997U 26145.24667715 +.00000000 +00000-0 +36149-3 0 00002
2 48997 87.9108 233.3268 0001900 93.2596 266.8752 13.16593241 04
| Epoch (UTC): | 25 May 2026 05:55:12 |
| Eccentricity: | 0.0001900 |
| inclination: | 87.9108° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3268° |
| argument of perigee: | 93.2596° |
| revolutions per day: | 13.16593241 |
| mean anomaly at epoch: | 266.8752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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