▸Orbital parameters

Orbit class	SSO
Inclination	98.1279°
Eccentricity	0.0001536
Period	98.4 min
Apogee	683 km
Perigee	681 km
Mean motion	14.63384435 rev/day
RAAN	194.9938°
Arg of perigee	97.4375°
Mean anomaly	262.7001°
B*	8.0383e-5
Rev at epoch	61,054

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 40376U 15003A 26188.18242250 .00000369 00000-0 80383-4 0 9992

2 40376 98.1279 194.9938 0001536 97.4375 262.7001 14.63384435610546

▸ source OMM (JSON)

{
  "OBJECT_NAME": "SMAP",
  "OBJECT_ID": "2015-003A",
  "EPOCH": "2026-07-07T04:22:41.304+00:00",
  "MEAN_MOTION": 14.63384435,
  "ECCENTRICITY": 0.0001536,
  "INCLINATION": 98.1279,
  "RA_OF_ASC_NODE": 194.9938,
  "ARG_OF_PERICENTER": 97.4375,
  "MEAN_ANOMALY": 262.7001,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 40376,
  "REV_AT_EPOCH": 61054,
  "BSTAR": 0.000080383,
  "MEAN_MOTION_DOT": 0.00000369,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	SMAP
Operator	Jet Propulsion LabHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree Jet Propulsion LaboratoryMEDIUMvia Wikidata
Country	United States
Launch date	Jan 31, 2015HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	944HIGHvia GCAT — Jonathan McDowell's General Catalog

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/40376

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.