▸Orbital parameters

Orbit class	SSO
Inclination	97.2272°
Eccentricity	0.0001802
Period	93.5 min
Apogee	445 km
Perigee	443 km
Mean motion	15.40647671 rev/day
RAAN	278.3913°
Arg of perigee	132.2744°
Mean anomaly	227.8656°
B*	2.8267e-6
Rev at epoch	8,256

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 62631U 25009Y 26187.72523014 .00000035 00000-0 28267-5 0 9990

2 62631 97.2272 278.3913 0001802 132.2744 227.8656 15.40647671 82564

▸ source OMM (JSON)

{
  "OBJECT_NAME": "PELICAN-2",
  "OBJECT_ID": "2025-009Y",
  "EPOCH": "2026-07-06T17:24:19.884+00:00",
  "MEAN_MOTION": 15.40647671,
  "ECCENTRICITY": 0.0001802,
  "INCLINATION": 97.2272,
  "RA_OF_ASC_NODE": 278.3913,
  "ARG_OF_PERICENTER": 132.2744,
  "MEAN_ANOMALY": 227.8656,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 62631,
  "REV_AT_EPOCH": 8256,
  "BSTAR": 0.0000028267,
  "MEAN_MOTION_DOT": 3.5e-7,
  "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	PELICAN-2
Operator	Planet Labs, Inc. (Planet)HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jan 14, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	160HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/62631

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