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 37951U 26145.61681346 +.00000000 +00000-0 +00000-0 0 00001
2 37951 8.6995 74.1358 0002394 353.3047 204.9273 1.00268556 05
| Epoch (UTC): | 25 May 2026 14:48:12 |
| Eccentricity: | 0.0002394 |
| inclination: | 8.6995° |
| perigee height: | 35777 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 74.1358° |
| argument of perigee: | 353.3047° |
| revolutions per day: | 1.00268556 |
| mean anomaly at epoch: | 204.9273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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